This procedure covers ultrasonic inspection of tubular, centrifugally-cast, corrosion-resistant steel cylinders. This procedure has been used typically for locating defects such as cracks, voids, spongy areas, and other discontinuities, but usage is not limited to such applications. This procedure is not applicable to austenitic steels where grain boundaries mask results. Immersion inspection is applicable to tubular products whose wall thickness is 0.5 to 9.0 inches (13 to 229mm). Contact inspection is applicable to tubular product whose wall thickness is 3.0 to 9.0 inches (76 to 229 mm).

This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy forgings. Premium grade is a term used to describe titanium alloys used for critical rotating components in turbine engines. For details, see SAE AMS2380, the specification that covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.

This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy forgings. Premium grade is a term used to describe titanium alloys used for critical rotating components in turbine engines. For details, see SAE AMS2380, the specification that covers the procedures for approval of products of premium-quality titanium alloys and the controls to be exercised in producing such products.

This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of 1-1-84. It is recommended that this specification not be specified for new designs. This cover sheet should be attached to the initial issue of the sUbject specification. Noncurrent refers to those procedures which have previously been widely used and which may be required on some existing designs in the future. The Aerospace Materials Division does not recommend these as standard procedures for future use in new designs. Each of these "Noncurrent" specifications is available from SAE upon request. This specification has been CANCELLED by the Aerospace Materials Division, SAE, as of August, 1989. By this action, subject specification number and its title will be deleted from the active specification index of Aerospace Material Specifications.

This Aerospace Standard establishes an identification system and provides design and tolerance information in describing two series of image quality indicators currently used in radiography of aerospace components, especially in electronic component evaluation and radiographic film and paper classification.

This Aerospace Standard establishes an identification system and provides design and tolerance information in describing two series of image quality indicators currently used in radiography of aerospace components, especially in electronic component evaluation and radiographic film and paper classification.

This recommended practice establishes the requirements and procedures for Barkhausen Noise (BN) inspection of ferromagnetic steel components. Applications of the method are listed below in 1.2 through 1.5.